Suffered a mishap on landing. The nose gear would not come down. The pilot tried everything to get it down, no luck. It was decided he would land on the runway and keep his nose up as long as he could. There was some concern the external wing tanks would drag so of course the crash trucks were there in case of fire. The pilot brought the plane in very slowly and landed on the mains, kept the nose up and almost came to a stop before the nose dropped. The radome was of course scraped up, the ring around the intake and the lower tacan antenna was gone. The wing tanks were about 5-6 inches from the ground. It was found out the seals in the nose gear were almost totally deteriorated. It was the original nose gear from the factory. Everything that was damaged was replaced and the plane was flying three days later. Anyone who knows the exact date, please let us know.

Update: A visitor wonders if this was the mishap involving pilot Dick Hoover who could not get the nose gear down at a Red Flag exercise, but also was not sure about the exact date.

Went down over the Gulf of Mexico off the coast of Florida. The crash was caused by an N2 speed sensor fault due to failed pins inside the sensor. The aircraft was recovered but damage was extensive to the cockpit area. The aircraft remains were brought back to MacDill AFB and stored in a hanger with the front being replaced by the front of #84-1228. Everything was removed forward of the intake and it was used as a maintainance trainer for a while.

At 1:09 local time the main generator warning light came on and the EPU started. The pilot Major John Cary who was part of a four ship flight advised of his emergency and tried to make it to Buckley ANGB. After flying in for five minutes on the EPU, that failed and flight controls were lost. Major Cary ejected at 1000 feet with a 90 degree nose down near Elizabeth, Colorado. Injuries were sore neck, chipped tooth and swollen eye which resulted in temporary blindness. This was caused by the high negative G's the aircraft pulled (-6G during a pitch down). The reason for the failure was due to an EPU overspeed which caused an over voltage to the flight control computer causing it to shut down.

Aircraft was damaged beyond repair when it ran over the barrier at Leeuwarden AB, the Netherlands. The pilot, Lt. Filip Appeldorn, ejected safely and survived the accident. The mishap occurred during initial conversion training due to an engine problem. This was the first zero-zero ejection from an F-16

Crashed in the Utah Test & Training Range, killing the pilot, Captain J. Edgington Moats at 14:54 hours. All USAF F-16's were grounded two days later. It was the F-16's second grounding. Cause of accident was a malfunctioning bleed air valve which allowed bleed air to leak out onto the EPU, causing an electrical surge that shut down the flight control computer. The pilot initiated ejection, but was too late.